SL-16 DEB, 39302

Orbit data source: Space-Track

SL-16 DEB, 39302 is space debris in LEO originally from a launch on Fri, 25 Dec 1992 UTC launched from the Tyuratam Missile And Space Complex (TTMTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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https://www.satcat.com/sats-embedded/39302?theme=dark&initialShowStats=false

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Identifier

39302, 1992-093JT

Orbit

LEO

Country

CIS

Related business

Russian Strategic Rocket Forces (RU)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1992-12-25 (33 years ago)

Launch vehicle

Unknown

Launch site

Tyuratam Missile And Space Complex (TTMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.1 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 2 weeks ago

TLE from 2 weeks ago

0 SL-16 DEB
1 39302U 92093JT  25341.43201890  .00013445  00000-0  47759-2 0  9993
2 39302  70.9834  44.2079 0123979 251.7179 123.8626 14.30255912630840

Epoch: 2025-12-07T10:22Z

TLE epoch observation values (Epoch: 2025-12-07T10:22:06.432Z)

Latitude

15.80006°

Longitude

177.80278°

Altitude

842.899 km

Speed

7.407 km/s

True Right ascension

03h 19m 06s

True Declination

15° 42' 41"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

16:22:57

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

877.641 km

Perigee altitude

699.932 km

Semi-major axis

7,166.924 km

Eccentricity

0.0124

Inclination

70.9834°

RAAN

44.2079°

Arg. of periapsis

251.7179°

True anomaly

125.03213°

Mean anomaly

123.8626°

Eccentric anomaly

124.44838°

Mean motion

3.57721 °/min

Orbital period

100.64 mins

BSTAR

0.0047759

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Other satellites on launch #93 in the year 1992 (1992-12-25 UTC)

SL-16 DEB, 39858 (Decayed)

SL-16 DEB, 22468 (Decayed)

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SL-16 DEB Visibility forecast

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Span	Click to sort rows by Start time (UTC) header in descending order	Start Az.	Max El. time (UTC)	Max El. Az.	Max El.	End time (UTC)	End Az.
10 mins	2025-12-19 02:41:06.207Z	168.252° S	2025-12-19 02:46:06.207Z	98.325° ESE	31.435°	2025-12-19 02:51:06.207Z	39.295° NE
8 mins	2025-12-19 04:25:06.207Z	248.76° W	2025-12-19 04:29:06.207Z	308.652° NW	28.141°	2025-12-19 04:33:06.207Z	0.256° NNE
5 mins	2025-12-19 11:32:06.207Z	24.749° NE	2025-12-19 11:34:06.207Z	48.739° ENE	14.963°	2025-12-19 11:37:06.207Z	83.344° E
8 mins	2025-12-19 13:14:06.207Z	333.843° NNW	2025-12-19 13:18:06.207Z	198.789° SSW	44.247°	2025-12-19 13:22:06.207Z	162.75° S

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Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out SL-16 DEB, 39302 on other resources

View SL-16 DEB, 39302 on Heavens-Above

View SL-16 DEB, 39302 on Keep Track

View SL-16 DEB, 39302 on Celestrak

View SL-16 DEB, 39302 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

SL-16 DEB, 39302

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 weeks ago

TLE from 2 weeks ago

TLE epoch observation values (Epoch: 2025-12-07T10:22:06.432Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #93 in the year 1992 (1992-12-25 UTC)

SL-16 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out SL-16 DEB, 39302 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 2 weeks ago